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Wind-tunnel investigation of the effects of horizontal-tail position on the low-speed longitudinal stability characteristics of an airplane model with a 35 degrees sweptback wing equipped with chordwise fencesAn experimental investigation was made in the Langley stability tunnel to determine whether the low-speed longitudinal stability characteristics of a model with a 35 degree sweptback wing could be improved appreciably by lowering the horizontal tail. The investigation included tests of several components of the model and of various model configurations with chordwise fences on the wing.
Document ID
19930086818
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Queijo, M J
Wolhart, Walter D
Date Acquired
August 29, 2013
Publication Date
November 5, 1951
Report/Patent Number
NACA-RM-L51H17
Report Number: NACA-RM-L51H17
Accession Number
93R16108
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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